A review of hybrid-electric energy management and its inclusion in vehicle sizing

Traditional aircraft sizing and optimization methods have been modified to account for various forms of non-gas turbine propulsion systems. While many of these methods do not include energy management into the actual sizing and optimization process, they still provide useful starting points for incl...

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Bibliographic Details
Published in:Aircraft Engineering and Aerospace Technology 2014-11, Vol.86 (6), p.550-557
Main Authors: Perullo, Christopher, Mavris, Dimitri
Format: Article
Language:English
Subjects:
Aircraft
Aircraft components
Aircraft design
Aircraft performance
Airplane engines
Design
Design optimization
Electric propulsion
Electric vehicles
Energy consumption
Energy management
Energy resources
Energy storage
Fly by wire control
Fuel cells
Gas turbines
Hybrid electric vehicles
Hybrid propulsion systems
Hybrid vehicles
Hybridization
Linear algebra
Mathematical models
Methods
Modelling
Optimization
Predictive control
Sizing
Storage systems
Studies
Turbines
Variables
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Summary:Traditional aircraft sizing and optimization methods have been modified to account for various forms of non-gas turbine propulsion systems. While many of these methods do not include energy management into the actual sizing and optimization process, they still provide useful starting points for inclusion of energy management into the optimization. Martins (2013) divides the optimization problem into two distinct classifications, monolithic and distributed architectures.
ISSN:0002-2667
1748-8842
1758-4213
DOI:10.1108/AEAT-04-2014-0041